Structural Optimization and Aeroelastic Analysis of a Subsonic Flying Wing Configuration

被引：0
|
作者：
Li, Liang [1 ]
Sun, Qin [1 ]
机构：
[1] Northwestern Polytech Univ, Xian 710072, Shaanxi, Peoples R China
来源：
PROCEEDINGS OF THE FOURTH INTERNATIONAL CONFERENCE OF MODELLING AND SIMULATION (ICMS2011), VOL 2 | 2011年
关键词：
flying wing; structural optimization; aeroelatic analysis;
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
In this paper, a flying wing model is developed, including structural finite element model and aeroelastic model, and then is made structural optimization and aeroelastic analysis. Throich structural optimization with different constraints and material selections, and aeroelastic analysis, some valued conclusions are achieved, which are useful for future flying wing design.
引用
收藏
页码：155 / 158
页数：4
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